A method of reducing the severity of the thermal stress state in blades of gas turbine engines by selecting the optimum distribution of the thickness of a ceramic thermal barrier c... von TRET'YACHENO, G. N, GRIBKOV, YU. A, KARPINOS, B. S, SAMULEEV, V. V

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TITANIUM-BASE ALLOY von SLOBTSOV P.I, MOISEEV V.N, GRIBKOV YU.A, TETYUKHIN V.V, KHOREV A.I, TRUBIN A.N, KOZLOVA F.I, ANTIPOV A.I, LISSOV V.K, LEVIN S.K

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